1) In the ATA 100 zonal system, the passenger entry door will have a designation of Report

800.

600.

400.

2) Which area of the aircraft is subject to hoop stress Report

Control surfaces.

Pressure cabin.

Wings.

3) Shear stress is described as the Report

pulling forces.

compressing forces.

slip away under the action of forces.

4) The aircraft grounding cable should be a Report

single strand copper wire, 0.5 in. cross sectional area.

copper stranded 0.5 in. cross sectional area.

single strand 18 AWG.

5) A job card identifies a location of a coponent in an aircraft by FS245, RWS45. This means Report

245 inches from the nose of the aircraft and 45 inches from the tip of the right wing.

245 inches from the datum line of the aircraft and 45 inches from the centreline of the right wing.

245 inches from the nose of the aircraft and 45 inches from the centreline of the right wing.

6) How is the radome protected from lightning strike Report

Special grease on the hinges.

Diverter strips.

Special paint.

7) If you short the two prongs with the single prong of a bonding tester together, what would the gauge read Report

Full scale deflection.

Centre scale.

Zero.

8) The force that cuases a permanent deformation of a material is known as Report

Stress

Strear

Strain

9) Semi-monocoque construction Report

utilizes the safe-life design concept.

is used only for the fuselage.

offers good damage resistance.

10) Most of the aircraft radio aerials are Report

bonded.

not bonded.

insulated from the fuselage.

11) Secondary bonding is usually provided with Report

stranded copper 0.25 inch.

single strand 0.25 inch.

Single wire 18 AWG (American wire gauge)

12) Water Lines (WLs) are measured points on Report

vertical line.

wing line.

horizontal line.

13) Water Lines are measured from Report

Vertical line

Horizontal line

Wing line

14) The various parts of the airframe are maintained at the same potential by Report

bonding.

earthing.

static wicks.

15) The cross sectional area of a secondary conductor must be not less than Report

18 SWG for a single wire.

22 SWG x 0.25.

22 SWG x 0.5.

16) What governs the ultimate fatigue life of an aircraft? Report

Pressure Cycles.

Flying Hours.

Number of Landings.

17) Aircraft structure is subjected to what types of stresses? Report

tension, compression, torsion and shear.

tension, compression, torsion and strain.

tension, compression, twisting and shear.

18) What determines the life of an aircraft structure Report

Number of landings.

Pressurization cycle.

Flying hours.

19) Imaginary vertical line from which all the lateral measurements are taken is known as Report

Buttock line

Water Line

Datum Line

20) What are buttock lines Report

Measurements from the centre line.

Horizontal measurement lines.

Vertical measurement lines.

EASA Questions Module 11 Set 1: Theory Of Flight

Set 1: Theory of flight

Set 2: Airframe Structures

Set 3: Aeroplanes-Fuselage

Set 4: Cabin Pressurisation

Set 5: Instruments

Set 6: Avionic system

Set 7: Avionic system

Set 8: Navigation

Set 9: Electrical Power

Set 10: Electrical System

Set 11: Battery

Set 12: Equip & Furnishing

Set 13: Fire Protection

Set 14: Fuel Systems

Set 15: Hydraulic Power

Set 16: Ice & Rain

Set 17: Flight Controls

Set 18: Flight Controls_1

Set 19: Landing Gear

Set 20: Lights

Set 21: Oxygen

Set 22: Pneumatic

Set 23: Water & Waste